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roswell

Office of the Secretary of Defense · 993 pages · text from the file's own layer

The Roswell Report: Fact versus Fiction in the New Mexico Desert was published in 1995 by Headquarters United States Air Force. It was written in response to Representative Steven H. Schiff's request and a General Accounting Office audit, and it contains Col. Richard L. Weaver's report and 1st Lt. James McAndrew's synopsis, along with attachments, appendices and photographs. The report says researchers found no evidence of an extraterrestrial craft or crew. It concludes that the 1947 debris came from a Project MOGUL balloon train.

  • p. 17 …Others remain nonbelievers or at least skeptical of the existence of alien beings and elusive vehicles…
  • p. 19 …Moreover, operational necessity required that these balloons be launched during daylight hours. It was therefore not…
  • p. 30 …This has since grown from a minimal amount of debris recovered from a small area to…
  • p. 35 …This included, for example, a small amount of missing "decimal files" from the 509th Bomb Group…
  • p. 36 …This was a small section of the July Historical Report for the 509th Bomb Group and…
  • p. 37 …To believe that such operational and high-level security activity could be conducted solely by relying…
  • p. 39 …The foil-rubber material could not be tom like ordinary aluminum foil can be tom... " Sally…
  • p. 40 …Although there does not appear to be much dispute that Cavitt was involved in the material…
  • p. 43 …Lt Col Cavitt described a small area of debris which appeared, "to resemble bamboo type square…
  • p. 72 …being per:ormed on these bodies. The bodies were described as the body of a small…
  • p. 99 …It should be noted that the period from approximately 1946 to 1950 is the least well…
  • p. 105 …Several small projects were completed during ~1e mont.~ includine signs on all the·office doors, a…
  • p. 149 …Streett 1s office recaumends against it on the ground that that is a small enterprize down…
  • p. 159 …I do not recall the incident being mentioned again as being any big deal and I…
  • p. 201 …We even simulated a small lightning strike over dry snow (just from the snow blowing over…
  • p. 258 …Big plastic balloon with small auxiliary plastics," etc. "Watson Lab and gear." "Followed" (inaudible) "receiver until…
  • p. 261 …explain bodies or material that can't be folded) by a sledge hammer. Q: Let's…
  • p. 328 …The witnesses have recalled small pink/purple "flowers" that appeared I to be some sort of…
  • p. 401 …b7 how ra* the receiver •7 be re110ve~ .t'rows the pre~er. red height withqut…
  • p. 443 …geostrophic wind (the latter being derived under certain simplifying assumptions) and since the geometry of the…
  • p. 458 …Two designs which compro- mise extreme cost (required for balloons of high internal pressure) with small…
  • p. 479 …This means that several hours might be required to fall through the lanes of aircraft traffic…
  • p. 484 …The change in drag effect may be realized by a decrease of relative size of the…
  • p. 487 (a) Then: (9) or for small temperature differences: (10) : - _L (.AI.)1-B T the nega…
  • p. 490 …gas of a balloon can be lost by: leakage through small holes in the fabric or…
  • p. 491 …for l:n•y small section of altitude is assumed to be constant); and re.J…
  • p. 506 in the preceding, section on diffusion end leakage the appendix opening should be small. It can…
  • p. 521 …is li~ited as indicated above, small variations may be detected with the result that it…
  • p. 555 …being exposed about 10 hours at cold temperature. (:S) During the floating period :many small oscilla…
  • p. 565 …The very usef.ul information about be.llast flow was reported clearly, and the principle of…
  • p. 566 …Since the small external appendix with cardboard stiffeners was not suitable for the large balloon, a…
  • p. 580 …Following the initial activation at about 38,500 feet, small oscillations were introduced into the flight…
  • p. 614 …Figure 4 shows this appendix construction on a General M lls balloon which is being inflated…
  • p. 652 …At high altitudes, a difference of 40°C may be expected in the temperature of the…
  • p. 658 …To facilitate handling of the line segments each length is prepared with a small hook on…
  • p. 672 signals may be arranged so as to consume a very small portion of -transmission time. D…
  • p. 738 …These values may be compared with a diffusion loss of lift of the order of magnitude…
  • p. 742 …The constancy of level will be better the lower the diffusion and the lower, therefore, the…
  • p. 762 …te .::mrcht:.se of small item£. A furth..:r rec:uest ~s been subr:rl tte…
  • p. 783 …be of such a valve that with a large r~diosonde frequency variation for a small…
  • p. 785 …It is expected that this equipment will be flown about 8 l-1ay. A description of…
  • p. 815 …Before gear could be recovered, most of it had be~~tolen. Stations operating at north hanger…
  • p. 842 …Range started to slowly increase as did elevation with azimuth being stationary. The echo remained beyond…
  • p. 862 …By using this stressed tape design, much larger loads may be carried than the thin polyethylene…
  • p. 874 …At this point, two small holes about 18" apart have been made, and the rip line…
  • p. 881 …If thodolite stadia determinations are being made, the banner can be used as one of the…
  • p. 898 …laid out, A small amount of gas at very low pressure Should be valved into the…
  • p. 910 …The motor gears may be cleaned with carbon tetrachloride and a small clean brush. If the…
  • p. 918 …Each combination of dots or dashes may be identified by ear, and with a calibration chart…
AUGUST 1948 AT HE L STAN F. S PI L HAC S, C. S. S C H ~EIDER, A~ D C. B. l\1 0 0 R E 133
capsule and linkage is of conventional design but in
place of the commutator bar, a motor driven helix is
employed. This system permits the determination of
FIG. 4. Minimum pressure switch (mercurial).
pressure data without knowledge of the history of con-
tact sequence or of the ascent or descent of the balloon,
as is required in the conventional radiosonde.
5. Tracking of the balloon
The balloons that have been flown by the writers
usually have been tracked by theodolites. Airplanes
have also been used, to extend the observations. These
two methods require the balloon to be visible and not
obscured by cloud cover. When available, ground
radar has been used in tracking the balloons, with
good results.
A series of SCR 658 radio direction-finders is also
used, arranged in a net along the expected trajectory
of the balloon. In addition, aircraft equipped with
inverted search radar have been employed to extend
the tracking net.
6. Flight results
While the characteristics of various plastics were
being investigated, four preliminary flights were made
with clusters of ordinary meteorological balloons, from
16 to 26 in number, to which two to four towing
balloons were attached. The towing balloons were cut
free by a baroswitch at a predetermined altitude. The
remainder of the balloons were inflated so that they
exactly balanced the load hung from the cluster. To
offset diffusion, sand was dropped from an arrange-
ment of tubes, 9 to 16 in number, each containing
about 200 to 1500 grams of sand ballast. This ballast
was dropped by a baroswitch mechanism on descent
only. Some of these flights were relatively successful
as a beginning method but the dropping of discrete
quantities of sand caused too great fluctuation of alti-
tude and therefore was abandoned later. The first
successful flight stayed at 51,000 ft, plus or minus 100
ft, ·for 38 minutes; another remained between 30,000
and 40,000 ft for 147 minutes. The latter shows the
same characteristic time-altitude curve as the cosmic-
ray clusters, although its altitude control is superior.
It is not believed that much improved altitude control
can be obtained, utilizing ordinary meteorological bal-
loons. Flight termination was usually due to deteriora-
tion of the balloon caused by the sun.
In the first flight utilizing plastic balloons, a cluster
of ten seven-foot diameter balloons6 was used. The
load on the cluster was 16.5 kilograms. An altitude
control was used. Unfortunately, the maximum alti-
tude reached was not as high as the predetermined
altitude which was selected to seal the diaphragm of
the automatic ballast valve. As a result, the cluster
rose to ceiling and stayed at this altitude for a short
while. Diffusion and leakage of helium produced a loss
of lift at the rate of 125 feet per minute.
The next flight was made with a single polyethylene
balloon, 15 ft in diameter. To insure sealing-off, the
ballast-release diaphragm was set to operate at an
altitude of 12,000 ft, considerably below the calculated
ceiling of the balloon. After a dawn release the balloon
continued to ascend to 15,100 ft where it leveled off,
then slowly descended to 9000 ft due to diffusion
losses. At this altitude the ballast release began to
operate and thereafter the balloon maintained its
altitude within ± 1300 ft for a period of 4! hours before
the radio signal was lost. However, in the first two
hours of this period, before the convection currents
e Made by General Mills, Inc.
LOW DRAIN
ELECTRIC
MOTOR
DRIVING HELIX AT
ABOUT 2 RPM
SUITABLE
LIGHT WEIGHT
HOUSING TO
PROTECT
lt.ISTRUMENT
DURING !'LIGHT
-HELIX
PLUG TO HAVE
CONNECTIONS WIRED
TO EACH CONTACT ARM,
TO HELIX AND
TO MOTOR
FI<i . .'. Olland-cyde pr('ssure mmlulatur.

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FOIA release, from the osd collection. The PDF is mirrored here; the original link is under it. 993 pages are in the text index: search them above, or from the library's search.